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Wyświetlanie 1-10 z 35
Tytuł:
A Numerical Study of The Heat Transfer Intensification Using High Amplitude Acoustic Waves
Autorzy:
Rulik, S.
Wróblewski, W.
Powiązania:
https://bibliotekanauki.pl/articles/177492.pdf
Data publikacji:
2018
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
cavity noise
sound wave cooling
flow over a cavity
transient cooling
blade cooling intensification
Opis:
The current practice in the efforts aiming to improve cooling conditions is to place emphasis on the application of non-stationary flow effects, such as the unsteady jet heat transfer or the heat transfer intensification by means of a high-amplitude oscillatory motion. The research presented in this paper follows this direction. A new concept is put forward to intensify the heat transfer in the cooling channels with the use of an acoustic wave generator. The acoustic wave is generated by a properly shaped fixed cavity or group of cavities. The sound generated by the cavity is a phenomenon analysed in various publications focused on the methods of its reduction. The phenomenon is related to the feedback mechanism between the vortices flowing from the leading edge and the acoustic waves generated within the cavity. The acoustic waves are generated by the interaction between the vortices and the cavity walls. Strong instabilities can be observed within a certain range of the free flow velocities. The investigations presented in this paper are oriented towards the use of the phenomenon for the purposes of the heat transfer process intensification. The first part of the work presents the numerical model used in the analysis, as well as its validation and comparison with empirical relations. The numerical model is constructed using the commercial CFD Ansys CFX-16.0 commercial program. The next part includes determining of the relationship between the amplitude of the acoustic oscillations and the cooling conditions within the cavity. The calculations are performed for various flow conditions.
Źródło:
Archives of Acoustics; 2018, 43, 1; 31-47
0137-5075
Pojawia się w:
Archives of Acoustics
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numerical estimation of losses in steam flow through LP turbine blade rows
Autorzy:
Dyskas, S.
Wróblewski, W.
Powiązania:
https://bibliotekanauki.pl/articles/1955213.pdf
Data publikacji:
2006
Wydawca:
Politechnika Gdańska
Tematy:
LP steam turbine
wet steam
condensation
losses
Opis:
The aim of this work is to estimate the losses in steam flow through an LP steam turbine rotor and the who]e stage. Two types of losses occur in steam flow, aerodynamic (profile, secondary flow, leakage) and thermodynamic (due to addition of heat caused by condensation). The presented numerical results are split into two groups. First, a comparison of three different calculation methods of steam flow is carried out. To this end, the geometry of an LP steam turbine's last rotor is chosen. The first examined method is the Streamline Curvature Method (SCM) used on the meridional plane with loss correlations, the other two being commercial and in-house CFD codes, solving the Reynolds-averaged Navier-Stokes equations for a 3D flow. The first two codes model equilibrium steam properties below the saturation line, while the latter models non-equilibrium steam properties. Finally, a comparison is made of the influence on lass prediction of various condensation models for the geometry of the penultimate stage, with the use of an in-house CFD code.
Źródło:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk; 2006, 10, 2; 177-190
1428-6394
Pojawia się w:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Numerical simulation of the blade cascade flows using upwind methods
Autorzy:
Chmielniak, T. J.
Wróblewski, W.
Powiązania:
https://bibliotekanauki.pl/articles/1953981.pdf
Data publikacji:
1998
Wydawca:
Politechnika Gdańska
Tematy:
numerical simulation
turbomachinery cascades
finite volume discretisation
upwind-biased technique
Opis:
A mathematical formulation of the equations of fluid motion in turbomachinery cascades has been presented. A review of the calculation methods for solving these equations is given. These methods are based on an explicit time marching scheme with finite volume discretisation and upwind-biased technique for the inviscid fluxes calculations. The high order accuracy in space is realized by the MUSCL approximation. The discretisation methods and numerical grids are described. The calculations of viscous and inviscid flow models are performed. The model and results of the water steam flow analysis with homogeneous condensation are presented. The calculations are performed for complex problems of real blade configurations of turbomachinery.
Źródło:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk; 1998, 2, 2; 287-317
1428-6394
Pojawia się w:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Experimental studies of leading edge vortex control of delta wing micro aerial vehicle
Autorzy:
Sibilski, K.
Żyluk, A.
Wróblewski, W.
Powiązania:
https://bibliotekanauki.pl/articles/246620.pdf
Data publikacji:
2018
Wydawca:
Instytut Techniczny Wojsk Lotniczych
Tematy:
MIcro Aerial Vehicles
unconventional control effectors
Opis:
It is known, that small disturbances generated by the micro actuators can alter large-scale vortex structures, and consequently, generate appreciable aerodynamic moments along all three axes for flight control. In the current study, we explored the possibility of independently controlling these moments. We perform analytical simulations showing optimal position of LEX generators, and water tunnel measurements showing effectiveness of MEX generators as MAV control devices. We applied array of actuators located on either the forward or the rear half section of the leading edge. Both one- and two-sided control configurations have also been investigated. Experimental results showed that asymmetric vortex pairs were formed, which leads to the generation of significant torques in all three axes. The article presents typical vortical flow over a delta wing, water tunnel at Wroclaw University of Technology, experimental setup and procedures, static test results on water tunnel testing including normal forces, pitching and yawing moments, maximum values of rolling, pitching, and yawing moment coefficients, effectiveness of pitching and yawing control.
Źródło:
Journal of KONES; 2018, 25, 3; 393-402
1231-4005
2354-0133
Pojawia się w:
Journal of KONES
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
A Numerical Study of the Relation Between the Acoustic Generator Geometry and the Heat Transfer Conditions
Autorzy:
Rulik, S.
Wróblewski, W.
Rusin, K.
Powiązania:
https://bibliotekanauki.pl/articles/140076.pdf
Data publikacji:
2018
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
cavity noise
cavity cooling
new cooling techniques
acoustic cooling
acoustic waves
heat transfer in cavities
thermoacoustics
szum aerodynamiczny
chłodzenie zewnętrzne
nowe techniki chłodzenia
chłodzenie akustyczne
fale akustyczne
przepływ ciepła
termoakustyka
Opis:
Modern gas turbine systems operate in temperatures ranging from 1200°C to even 1500°C, which creates bigger problems related to the blade material thermal strength. In order to ensure appropriate protection of the turbine blades, a sophisticated cooling system is used. Current emphasis is placed on the application of non-stationary flow effects to improve cooling conditions, e.g., the unsteady-jet heat transfer or the heat transfer enhancement using high-amplitude oscillatory motion. The presented research follows a similar direction. A new concept is proposed of intensification of the heat transfer in the cooling channels with the use of an acoustic wave generator. The acoustic wave is generated by an appropriately shaped fixed cavity or group of cavities. The phenomenon is related to the coupling mechanism between the vortex shedding generated at the leading edge and the acoustic waves generated within the cavity area. Strong instabilities can be observed within a certain range of the free flow velocities. The presented study includes determination of the relationship between the amplitude of acoustic oscillations and the cooling conditions within the cavity. Different geometries of the acoustic generator are investigated. Calculations are also performed for variable flow conditions. The research presented in this paper is based on a numerical model prepared using the Ansys CFX-17.0 commercial CFD code.
Źródło:
Archive of Mechanical Engineering; 2018, LXV, 1; 5-26
0004-0738
Pojawia się w:
Archive of Mechanical Engineering
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Metamodel-Based Optimization of the Labyrinth Seal
Autorzy:
Rulik, S.
Wróblewski, W.
Frączek, D.
Powiązania:
https://bibliotekanauki.pl/articles/140287.pdf
Data publikacji:
2017
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
labyrinth seal
metamodel optimization
neural network
genetic algorithm
evolutionary algorithm
CFD optimization
uszczelnienie labiryntowe
optymalizacja oparta na metamodelu
sieć neuronowa
algorytm genetyczny
algorytm ewolucyjny
optymalizacja CFD
Opis:
The presented paper concerns CFD optimization of the straight-through labyrinth seal with a smooth land. The aim of the process was to reduce the leakage flow through a labyrinth seal with two fins. Due to the complexity of the problem and for the sake of the computation time, a decision was made to modify the standard evolutionary optimization algorithm by adding an approach based on a metamodel. Five basic geometrical parameters of the labyrinth seal were taken into account: the angles of the seal’s two fins, and the fin width, height and pitch. Other parameters were constrained, including the clearance over the fins. The CFD calculations were carried out using the ANSYS-CFX commercial code. The in-house optimization algorithm was prepared in the Matlab environment. The presented metamodel was built using a Multi-Layer Perceptron Neural Network which was trained using the Levenberg-Marquardt algorithm. The Neural Network training and validation were carried out based on the data from the CFD analysis performed for different geometrical configurations of the labyrinth seal. The initial response surface was built based on the design of the experiment (DOE). The novelty of the proposed methodology is the steady improvement in the response surface goodness of fit. The accuracy of the response surface is increased by CFD calculations of the labyrinth seal additional geometrical configurations. These configurations are created based on the evolutionary algorithm operators such as selection, crossover and mutation. The created metamodel makes it possible to run a fast optimization process using a previously prepared response surface. The metamodel solution is validated against CFD calculations. It then complements the next generation of the evolutionary algorithm.
Źródło:
Archive of Mechanical Engineering; 2017, LXIV, 1; 75-91
0004-0738
Pojawia się w:
Archive of Mechanical Engineering
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Modelling of influence of turbulent transition on heat transfer conditions
Autorzy:
Bochon, K.
Wróblewski, W.
Dykas, S.
Powiązania:
https://bibliotekanauki.pl/articles/1943251.pdf
Data publikacji:
2008
Wydawca:
Politechnika Gdańska
Tematy:
laminar-turbulent transition
Conjugate Heat Transfer (CHT)
computational fluid dynamics CFD
Opis:
This article deals with the turbulent transition phenomenon modelling and its influence on heat transfer. The purpose of the analyses was to verify the transition modelling implemented in the ANSYS CFX 11 commercial code for popular test cases (low flow speed) described in literature, and then use it for verification of the in-house CFD code (created for compressible flows). The inhouse CFD code has been extended lately for the Conjugate Heat Transfer modelling (CHT) as well, taking into account important flow effects, especially the turbulent transition. A Wilcox k-omega turbulence model with the Low-Reynolds modification was used in the in-house code. The calculations in ANSYS CFX were made using an SST turbulence model and a gamma-theta transition model. A fully turbulent flow was modelled by means of both codes, and the results were compared with the available experimental data. Then, the turbulent transition for several test cases was analysed with ANSYS CFX. Afterwards, the in-house CFD code was verified by means of ANSYS CFX for a higher flow speed (Mach numbers). The CHT modelling was analysed by means of both codes and the results were compared and discussed. The conducted analyses show that the results obtained by means of both codes are comparable, but the turbulence model used in the in-house CFD code is simpler and requires less computation time. A modification of two equations turbulence models can be an alternative for design problems in more developed laminar/turbulent flows.
Źródło:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk; 2008, 12, 3-4; 173-184
1428-6394
Pojawia się w:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Application of hybrid CFD/CAA technique for modeling pressure fluctuations in transonic flows
Autorzy:
Dykas, S.
Wróblewski, W.
Rulik, S.
Powiązania:
https://bibliotekanauki.pl/articles/1955297.pdf
Data publikacji:
2013
Wydawca:
Politechnika Gdańska
Tematy:
transonic flow
aeroacoustic noise
hybrid technique
Opis:
Solving AeroAcoustics (CAA) problems by means of the Direct Numerical Simulation (DNS) or even the Large Eddy Simulation (LES) for a large computational domain is very time consuming and cannot be applied widely for engineering purposes. In this paper in-house CFD and CAA codes are presented. The in-house CFD code is based on the LES approach whereas the CAA code is an acoustic postprocessor solving non-linearized Euler equations for fluctuating (acoustic) variables. These codes are used to solve the pressure waves generated aerodynamically by a flow over a rectangular cavity and by the vortex street behind a turbine blade. The obtained results are discussed with respect to the application of the presented numerical techniques to pressure waves modeling in steam turbine stages.
Źródło:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk; 2013, 17, 3-4; 145--154
1428-6394
Pojawia się w:
TASK Quarterly. Scientific Bulletin of Academic Computer Centre in Gdansk
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Analiza sprawności obiegu cieplnego ultra-nadkrytycznego bloku kondensacyjnego dla szeregowej konfiguracji skraplaczy
The influence of application of a serial condenser for the ultra-critical power unit
Autorzy:
Wróblewski, W.
Łukowicz, H.
Rulik, S.
Powiązania:
https://bibliotekanauki.pl/articles/173112.pdf
Data publikacji:
2013
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
obieg cieplny
ultra-nadkrytyczny blok kondensacyjny
skraplacz
thermal cycle
ultra-supercritical condensing unit
condenser
Opis:
Przedmiotem niniejszej analizy jest dobór parametrów oraz konfiguracji układu chłodzenia dla bloku ultra-nadkrytycznego o mocy 900 MW. Analizę pracy skraplacza oparto o amerykańską normę Heat Exchange Institute. Przedstawione badania obejmują porównanie dwóch wariantów układu chłodzenia, które dotyczą konfiguracji równoległej oraz szeregowej pracy skraplacza. Układ równoległy jest powszechnie stosowany, a rozdzielenie strumienia wody chłodzącej na poszczególne skraplacze bądź sekcje skraplacza daje w nich jednakowe warunki kondensacji. W przypadku konfiguracji szeregowej całkowity strumień wody chłodzącej przepływa szeregowo przez skraplacz pierwszy, a następnie trafia do skraplacza drugiego. Takie rozwiązanie w stosunku do układu równoległego powoduje wzrost sprawności obiegu wynikający z obniżenia całkowitego ciśnienia w skraplaczu. Konfiguracja szeregowa powoduje, że obniżeniu ciśnienia w pierwszej sekcji skraplacza towarzyszy nieznaczny wzrost ciśnienia w drugiej sekcji skraplacza. Stąd też pole powierzchni wymiany ciepła drugiej sekcji skraplacza jest często zwiększone w celu poprawy warunków kondensacji. Niniejsza praca stanowi uzupełnienie oraz rozszerzenie przedstawionych w literaturze analiz. Dotyczy to w szczególności dokładnego uwzględnienia wpływu straty wylotowej turbiny niskoprężnej na wartość uzyskiwanych przyrostów sprawności obiegu cieplnego w przypadku konfiguracji szeregowej pracy skraplacza.
The aim of this paper is the selection of parameters and configuration of the cooling system of 900 MW ultra-supercritical power unit. The performed analysis of the condenser was based on the Heat Exchange Institute standard. The presented studies include comparison of two variants of cooling water system. Both, the parallel and serial configuration of the condenser was investigated. Parallel cooling water system is widely used, and the separation of the cooling water stream into individual sections of the condenser or condensers give equal conditions of condensation. In the case of a serial configuration, the total flow of cooling water flows through the first condenser and then it goes to the second condenser. This causes the decrease of pressure in the first and increase of pressure in the second condenser. Hence, the heat exchange surface area of the second condenser is often increased to improve the conditions of condensation. This paper extends the analyzes presented in the literature. It particularly concerns the investigation of influence of the exhaust loss for obtained efficiency gains in case of the serial configuration of condenser.
Źródło:
Archiwum Energetyki; 2013, 43, 1/2; 117-127
0066-684X
Pojawia się w:
Archiwum Energetyki
Dostawca treści:
Biblioteka Nauki
Artykuł
Wyświetlanie 1-10 z 35

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